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Showing 1 to 20 of 158 for “"aeroelastic"”.

  1. Geometrically Nonlinear Aeroelastic Scaling

    Aeroelastic scaling methodologies are developed for geometrically nonlinear applications. The new methods are demonstrated by designing an aeroelastically scaled model of a suitably nonlinear full-scale joined-wing aircraft. The best of the methods produce scaled models that closely replicate the …

    vt Repository record for Geometrically Nonlinear Aeroelastic Scaling (opens in a new tab)

  2. Strain actuated aeroelastic control

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.

    mit Repository record for Strain actuated aeroelastic control (opens in a new tab)

  3. Aeroelastic modelling of gyroplane rotors

    … gyroplane accidents still remains unclear. The aeroelastic behaviour of autorotating rotors is a relatively unexplored problem and it has not yet been investigated as possible cause of the accidents. A mathematical model was created to simulate aeroelastic behaviour of rotors in autorotation. …

    glasgow Repository record for Aeroelastic modelling of gyroplane rotors (opens in a new tab)

  4. Aeroelastic behaviour of composite wings

    … investigations into the structural, dynamic and aeroelastic behaviour of composite wings. The study begins with a literature review where the development of aeroelastic tailoring and specific applications of the technology are discussed in detail. A critique of methods for the determination of …

    city-london Repository record for Aeroelastic behaviour of composite wings (opens in a new tab)

  5. Aeroelastic Analysis of Membrane Wings

    … 2-D VLM and a doublet lattice method. The aeroelasticity is studied by varying parameters affecting the flow as well as parameters affecting the structure. The parametric studies are performed for cases of constant angle of attack, plunge and, pitch and plunge. The response of the …

    vt Repository record for Aeroelastic Analysis of Membrane Wings (opens in a new tab)

  6. Reduced-order modeling of aeroelastic phenomena

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-12-04 without embargo terms

    uiuc Repository record for Reduced-order modeling of aeroelastic phenomena (opens in a new tab)

  7. Aeroelastic optimization of thin flapping structure

    We study the flow generated when a handheld fan is waved. This fluid-structure interaction problem is investigated through precision experiments, using an oscillating semi-circular elastic plate as a reduced analog model. The aerodynamic performance of the fans is systematically characterized for a …

    mit Repository record for Aeroelastic optimization of thin flapping structure (opens in a new tab)

  8. Towards optimal strain actuated aeroelastic control

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.

    mit Repository record for Towards optimal strain actuated aeroelastic control (opens in a new tab)

  9. Sensitivity analysis of wing aeroelastic responses

    Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelastic instability lie outside the operating range) is an integral part of the wing design process. Availability of the sensitivity derivatives of the various critical speeds with respect to shape …

    vt Repository record for Sensitivity analysis of wing aeroelastic responses (opens in a new tab)

  10. Identification of Transient Nonlinear Aeroelastic Phenomena

    Complex nonlinear aspects of aeroelastic phenomena include unsteady nonlinear aerodynamic loads, structural nonlinearities, as well as nonlinear couplings between the flow and the structural response. Nonlinearities in aerodynamic loads originate from unsteady shocks and/or flow separation. …

    vt Repository record for Identification of Transient Nonlinear Aeroelastic Phenomena (opens in a new tab)

  11. Aeroelastic Analysis of a Flexible Membrane Wing

    … research proposal is the investigation of the aeroelastic effects of a flexible lift augmentation system (LAS) wing. This research involves characterization of the forced vibration response of a wing appendage used to augment short field take off and landing (STOL) operations.</p> <p>Although …

    embry-riddle Repository record for Aeroelastic Analysis of a Flexible Membrane Wing (opens in a new tab)

  12. Nonlinear Analysis and Control of Aeroelastic Systems

    … may lead to limit cycle oscillations (LCOs) in aeroelastic systems. LCOs can result in fatigue in wings leading to catastrophic failures. Existence of LCOs for velocities less than the linear flutter velocity has been observed during flight and wind tunnel tests, making such subcritical behavior …

    vt Repository record for Nonlinear Analysis and Control of Aeroelastic Systems (opens in a new tab)

  13. A mm-scale aeroelastic oscillation-based anemometer

    … By combining a 'fishtail'-shaped filament's aeroelastic and vortex-forced flutter modes, its oscillation frequency can be confined to scale smoothly with fluid velocity. This principle has been used to produce a low-cost, mm-scale anemometer that measures air flow to ±(5% + 0.5m/s) from …

    mit Repository record for A mm-scale aeroelastic oscillation-based anemometer (opens in a new tab)

  14. Aeroelastic study of a multi-hinged wing

    Dynamic aeroelastic response of multi-segmented hinged wings is studied theoretically and experimentally in this thesis. For the theoretical study, a method of modeling the aeroelastic characteristics of multi-hinged wings is proposed. The method employs the Runge-Kutta scheme to solve the …

    mit Repository record for Aeroelastic study of a multi-hinged wing (opens in a new tab)

  15. It’s Not Just a Phase: Real-Time Aeroelastic Flutter Control Optical Flow Sensing and Piezoelectric Control of Aeroelastic Flutter

    Aeroelastic flutter poses a critical threat to aircraft safety, occurring when aerodynamic forcescouple with structural dynamics to create potentially catastrophic, self-amplifying oscillations that lead to structural failure. Traditional active flutter detection and control methods rely on …

    unr Repository record for It’s Not Just a Phase: Real-Time Aeroelastic Flutter Control Optical Flow Sensing and Piezoelectric Control of Aeroelastic Flutter (opens in a new tab)

  16. Experimental and numerical study of hypersonic aeroelastic intakes

    … the off-design intake operations due to aeroelasticity. An aeroelastic intake was tested in a hypersonic wind tunnel to assess its dynamic flowfield, structural response, and performance. The experiments were informed with static 2D, full-scale static 3D, and fully coupled 2D and 3D …

    unsw Repository record for Experimental and numerical study of hypersonic aeroelastic intakes (opens in a new tab)

  17. A CFD framework for aeroelastic gust load calculations

    … (CFD) framework for the simulation of the aeroelastic response of aircraft flying under gust loading was developed. The multiphysics, Finite Volume, VertexCentered code Elementaltextsuperscript{textregistered} was employed and calculations were performed for the transonic flow regime. In …

    cape-town Repository record for A CFD framework for aeroelastic gust load calculations (opens in a new tab)

  18. Aeroelastic studies on a high aspect ratio wing

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.

    mit Repository record for Aeroelastic studies on a high aspect ratio wing (opens in a new tab)

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